发明名称 Thermal Management For Aircraft Composites
摘要 A composite article including a fiber-reinforced resin composite having an internal portion, and an internal surface and an external surface; and a thermal article formed of an anisotropic graphite sheet having a thermo-mechanical design constant of at least 10 mm-W/m*K, the thermal article positioned in the internal portion of the fiber-reinforced resin composite, wherein the thermo-mechanical design constant of a material is defined by thermal conductivity of the material multiplied by its average thickness.
申请公布号 US2013280470(A1) 申请公布日期 2013.10.24
申请号 US201213451904 申请日期 2012.04.20
申请人 NORLY JULIAN 发明人 NORLY JULIAN
分类号 B32B1/06 主分类号 B32B1/06
代理机构 代理人
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